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固体弹道导弹级间热分离特性研究
引用本文:孔丽,孙建国,戴宇进,李红亮. 固体弹道导弹级间热分离特性研究[J]. 海军航空工程学院学报, 2009, 24(6): 617-621
作者姓名:孔丽  孙建国  戴宇进  李红亮
作者单位:海军航空工程学院飞行器工程系,山东,烟台,264001;海军航空工程学院新装备培训中心,山东,烟台,264001;海军航空工程学院,七系,山东,烟台,264001;海军航空工程学院研究生管理大队,山东,烟台,264001
摘    要:
根据某型导弹级间分离的要求,建立了级间热分离模型,研究了不同条件下固体导弹级间热分离特性,并用MATLAB软件进行模拟运算,给出了固体导弹级间热分离的主要影响因素,为导弹总体优化设计提供了有力的支持。

关 键 词:固体导弹  级间热分离  分离特性

Research on Stage-Separation Characteristics for Solid-Propellant Ballistic Missile
KONG Li,SUN Jian-guo,DAI YU-jin and LI Hong-liang. Research on Stage-Separation Characteristics for Solid-Propellant Ballistic Missile[J]. Journal of Naval Aeronautical Engineering Institute, 2009, 24(6): 617-621
Authors:KONG Li  SUN Jian-guo  DAI YU-jin  LI Hong-liang
Affiliation:d (. Naval Aeronautical and Astronautical University a. Department of Airborne Vehicle Engineering; b. New Equipment Training Center; c.No.7 Department; d. Graduate Students' Brigade, Yantai Shandong 264001, China)
Abstract:
In this paper,thermal stage separation model was built based on the requirements to stage seperation of a certain type of missile,and solid missile's thermal seperation characteristics were studied under dissimilar conditions,and were simulated by using MATLAB.Main factors were presented which affected solid missile's thermal stage separation,powerful support was provided for missile system optimizing design.
Keywords:solid missile  thermal stage separation  seperation characteristic  
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